theoretical analysis of a dipole-fed horn antennadiscontinuities to be included in the horn geometry...

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First International Symposium on Space Terahertz Technology Page 187 THEORETICAL ANALYSIS OF A DIPOLE-FED HORN ANTENNA G.V. Eleftheriades, Walid Ali-Ahmad, L.P.B. Katehi, G.M Rebeiz Center for Space Terahertz Technology, University of Michigan, Ann Arbor, MI March 1990 Abstract This antenna consists of a strip dipole printed on a membrane and suspended in an etched pyramidal silicon cavity. The entire fabrication is monolithic. For the theoretical character- ization, the horn is approximated by a stepped structure of multiple rectangular waveguicle sections. The fields in each section are given by a linear combinatión of waveguide modes, and the fields in air are given by a continuous plane wave spectrum. To evaluate the Green's function for this problem, an infinitesimally small electric dipole is considered in one of the waveguide sections. Then, the fields inside the silicon cavity are evaluated, and the far-field patterns are found from the Fourier transforms of the electric field on the aperture of the horn.

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  • First International Symposium on Space Terahertz Technology Page 187

    THEORETICAL ANALYSIS OF A DIPOLE-FED HORN

    ANTENNA

    G.V. Eleftheriades, Walid Ali-Ahmad, L.P.B. Katehi, G.M Rebeiz

    Center for Space Terahertz Technology,

    University of Michigan, Ann Arbor, MI

    March 1990

    Abstract

    This antenna consists of a strip dipole printed on a membrane and suspended in an etched

    pyramidal silicon cavity. The entire fabrication is monolithic. For the theoretical character-

    ization, the horn is approximated by a stepped structure of multiple rectangular waveguicle

    sections. The fields in each section are given by a linear combinatión of waveguide modes,

    and the fields in air are given by a continuous plane wave spectrum. To evaluate the Green's

    function for this problem, an infinitesimally small electric dipole is considered in one of the

    waveguide sections. Then, the fields inside the silicon cavity are evaluated, and the far-field

    patterns are found from the Fourier transforms of the electric field on the aperture of the

    horn.

  • Page 188 First International Symposium on Space Terahertz Technology

    1. INTRODUCTION

    In millimeter wave imaging systems the use of a single detector with electronic or me-

    chanical scanning is inadequate. The events may be too fast, or the required integration

    time too long. The way to eliminate this limitation is to image all points simultaneously.

    In 1987, G.M. Rebeiz fabricated a monolithic millimeter-wave imaging array consisting of a

    large number of silicon horns with detectors placed at the focal plane of the imaging system.

    For the design of this array, the radiating elements were characterized experimentally and

    mutual coupling was neglected. As a result, the efficiency of the array was approximately

    45 percent. To improve the performance of the array, the elements have to be modeled

    accurately. This paper presents the development of a rigorous method for the theoretical

    characterization of the isolated elements.

    The procedure for rigorously generating the Green's function for a dipole-fed metallic

    rectangular horn radiating in free-space is being described. The method allows for step

    discontinuities to be included in the horn geometry and is not limited by large flaring

    angles or short axial lengths.

    2. THEORY

    The procedure which has been employed in the formulation of the problem consists of

    five steps:

    1. The geometry of the horn is approximated by a cascade of rectangular waveguide

    steps. One of the waveguide steps contains an infinitesimal dipole excitation.

    2. The field on the apex and aperture of the horn is transfered, via appropriate trans-

    mission matrices, on the excitation (source) plane.

    3. The aperture field is matched to free space using plane-wave expansion.

    4. The transfered fields of step two are matched over the excitation plane.

    5. Finally steps (3) and (4) combined together result in a linear system of equations.

    The solution of this system provides the required Green's function in discrete form

    inside the horn and in continuous form in the half space.

  • First International Symposium on Space Terahertz Technology Page 189

    2.1 Approximation of the horn geometry

    The horn is approximated by a multistepped discontinuity consisting of N sections as

    shown in Figure 1.

    The horn aperture lies on an infinite-metallic screen. Furthermore, it is assumed that

    there is no reflection from the apex of the horn, since any reflection will be at cut-off.

    2.2 Transfer of the apex and Apperture Field on the source plane

    Each step discontinuity is characterized by a transmission matrix [Tb]

    B(2)

    D(2)

    A(2)

    61(2)

    = [Tbi (1)

    where the elements of the column matrices denote the unknown coefficients of the field next

    to the discontinuity. The field in each waveguide is represented in a modal expansion as

    shown below :

    004i) [-e TE(x, y) { A (;7:ione_,I,ncon

    , B(i) „0,)771) z}rnn

    m,,n

    y) Cti)ne—'41)nz e+')Vnz}] (2)

    - x Ht(i) • E [e.2)7,1TE (x, 074T E, A (i) pie p-y2.)r z

    m ,n

    + (x, — D (i) e"'Uz } ".mm mm mnmm

    where i takes the values 1 or 2.

    In the above representation both TE and TM modes are included to support the analysis

    of an arbitrary planar excitation current. A cascade of such transmission matrices, along

    with associated phase delay transmission matrices is used to transfer the apex and aperture

    field on the excitation plane :

    (3)

  • - apex apperture

    = [TB]0

    0

    -BII

    DLL

    An

    CH

    (4)= [TA]

    -B(N)

    D(N)

    A(N)

    C(N)

    F11 F12 F13 F12

    F21 F22 F21 F24

    0

    0(7)

    0

    0

    °I° (k2 V' • • (k k )eln(k ky)dkdkx y1_00 z xi3 x,rPqlijmn (8)

    Page 190 First International Symposium on Space Terahertz Technology

    Referring to fig.1, the source interface divides the source section #K into two subsections.

    one on the left, having length 1, and one on the right, having length 1 H . Accordingly, in

    equations (4) above, the modal coefficients of the left subsection are denoted with the index

    (I) and those of the right subsection with the index (II).

    2.3 Matching to Half space

    This task matches the discrete field spectrum of the aperture section of the horn to the

    continuous field spectrum of free space, over the horn aperture. The field in free-space is

    expressed as a plane wave superposition:

    1 00 oo yyE(x , y, z)f_

    , ky)e—ik ik e- ikzz dkrdky2r oo

    f

    with the transverse component of (lc, ky ) given by:

    (5)

    gt(k ky) =1

    27r I /apertureEt (x , y , 0+) e ik.rx ikyye dxdy

    Field continuity on the aperture of the horn leads to the following matrix equation

    The submatrices Fii contain reaction integrals involving the discrete modes of the aper-

    ture field. There are three kind of reaction integrals as shown below

  • B(H) 0

    D(II)

    A(H) ern(xi, YI)r-,(11)

    eInimn(xl

    (15)[A] = [A]

    First International Symposium on Space Terahertz Technology Page 191

    °13 r (k2 _ k!) e..7) (k kx y),e y*o x, y ) yk dk, dk (9)2ijmn00 — 00 Z

    /Pqkxky—[e • -(ks ky)e" (ks, ky)

    eP• •(

    kx,

    ky)

    e" (k k y Adk dk &Of))3ijmn 00 _00 kz yzj xmn ri ymn

    where p,q take the values 1 (—÷ TE) or 2 (---> TM).

    In order to facilitate the numerical evaluation of the integrals it is advantageous to

    transform them in the space-domain. Their transformation from the spectral-domain to

    the spatial-domain is accomplished via the application of Parseval's theorem leading to

    ITN TYN?. — (k2Jrv —)l mn ay2Lilt T

    N i—

    YN P

    [ePsiii (—x) eximm (x)j{ePx2ii (—y) el2mn(y)]dxdy

    pg . 1 fxN p N ie —ikp ,92

    213mn — (k2xN i— YN P

    ax2 Ylij( —X ) eylmn(X)]

    [e 2 ( — y) ev2mn(Y)NXdy (12)

    rpq 1 fxN ie—ikp[(ePi..(—x) eximn(x))1 3ijmn =

    `i " X N P axay Y

    ( ePy2ij( — Y) eqs2ii(Y)) ( eP X eYlmn(X))(ePT2ij(—Y)xlij ( —) eyq2mn(y)]dxdy (13)

    where p = Vx2 + y2.

    2.4 Matching on the source interface

    The point excitation is assumed to be a y-directed surface current given by:

    K(x,y) = 6(x — /)6(y — (14)

    Upon matching over the source interface we derive the matrix equation

  • B(1)

    Do-)

    B- (N)

    D(N)

    A(N)

    C(N)

    (17)= [TA]= [TB]0

    0appertureapex

    • Matching of the aperture field :

    [A] = [A]

    0

    ern,E ri (x' , y1)

    eLmn (x' ,

    (19)

    Page 192 First International Symposium on Space Terahertz Technology

    where matrix [A] above involves the mode admittances of the source section as shown

    below :

    0_yTE,K 0 y TE,K

    (16)

    _yTM,K Q y TM,K

    2.5 Derivation of the final system of equations

    The equations that have been generated so far are summarized below

    • Apex-aperture field transfered on the source plane through transmission matrices:

    B (N) 0

    D(N)=-_

    A(N ) 0

    C(N) 0

    ▪ Matching of the fields on the source interface

    [1] (18)

  • [-TEr \ -TM/ \ -TE/ \ -TMemnAx, y) x,y) emnAx,y) emn [TB] [S Ili 1]

    0

    eTmEri (x', yi)

    ernT

    14. (xl yi)

    (21)

    First International Symposium on Space Terahertz Technology Page 193

    The above equations are merged together to form a single matrix equation involving the

    modal coefficients of the apex and aperture sections

    DO-)

    {ill[T B y — [A][11

    A l B (N ) el

    0 [1] D(N) €2

    .4 (N) 0

    C(N) 0

    Note that the block-submatrix ([A][m]y consists only of the half first columns of [A][TE31.

    This is a consequence of the assumption of no reflections from the apex of the horn. Having

    found the modal coefficients of the apex and aperture sections, the Green's function inside

    the horn is represented as a discrete Fourier series whereas outside the horn as a Fourier

    integral. Specifically the transverse component of the Green's function for a y-directed

    current inside the horn can be represented in a quadratic form as shown below

    G t (x , y ,

    (20)

    In the above representation [SIM] is an appropriate submatrix of the inverse of the

    system matrix defined in (19).

    3. NUMERICAL RESULTS

    The aperture field and the far-field for a specific horn geometry has been evaluated. For

    this purpose the aperture coefficients are calculated from the solution of matrix equation

    (20). For a vertical point source only modes of the form (m,n) [ m=1,3,5, ... and n=0,2,4,

    ...] are excited. Numerical convergence for the far-field was achieved when TE and TM

    modes up to the order (7,7) were included. The magnitude of the co-polarized aperture field

  • Page 194 First International Symposium on Space Terahertz Technology

    shown in fig.4 is recognized to be a perturbed dominant mode field distribution. Furter-

    more,the utilization of both TE and TM modes in the theory enabled the calculation of the

    cross-polarized aperture field which has a level of -16dB for the case under consideration.

    The phase of the aperture field is depicted in fig.5. Of interest is the cross-polarization phase

    which divides the aperture ,along its geometrical axes of symmetry, into four quadrants.

    Each quadrant is out of phase with its adjacent quadrants.

    4. CONCLUSION

    This paper presented a rigorous method for the characterization of a monolithic horn

    antenna excited by an infinitesimal small dipole printed on a membrane. Using this method,

    the fields on the aperture of the silicon horn were evaluated and transformed to the Fourier

    domain in order to derive the far-field patterns. The developed method may easily be

    extended to compute input impedance and resonant properties of these radiating structures

    for feeding dipoles of finite size.

    5. AKNOWLEDGMENTS

    The work was sponsored by the Center for Space Terahertz Technology, the University

    of Michigan, Ann Arbor, MI.

  • First International Symposium on Space Terahertz Technology Page 195

    REFERENCES

    1. Thomas Wriedt, Karl-Heinz Wolff, Frint Arndt and Ulrich Tucholke "Rigorous Hy-

    brid Field Theoretic Design of Stepped Rectangular Waveguide Mode Converters In-

    cluding the Horn Transitions into Half-Space," IEEE Transactions on Antennas and

    Propagation, Vol. 37, No. 6, June 1989.

    2. Amir I. Zaghloul and Robert H. MacPhie, "Cross-Correlation Formulation of the

    Complex Power from Planar Apertures," Radio Science, Vol. 10, No. 6, pp. 619-624,

    June 1975.

    3. Robert H. McPhie and Amir I. Zaghloul, "Radiation from a Rectangular Waveguide

    with Infinite Flange-Exact Solution by the Correlation Matrix Method," IEEE Trans-

    actions of Antennas and Propagation, Vol. AP-28, No. 4, July 1980.

    4. Jose A. Encinar and Jesus Rebollar, "A Hybrid Technique for Analyzing Corrugated

    and Non-Corrugated Rectangular Horns," IEEE Transactions on Antennas and Prop-

    agation, Vol. AP-34, No. 8, August 1986.

  • (1)

    C(1)

    „so #1

    D(1) b1

    440-- B(2)a2 D(2)

    Y2

    %xh ...-0■■• A(2)

    1,ir c(2)

    ,g,0,0

    #2

    Page 196 First International Symposium on Space Terahertz Technology

    Fig.1 A waveguide step discontinuity.

  • First-section#1

    (Apex)

    excitationinterface

    Last-Section(#N)(Aperture)

    First International Symposium on Space Terahertz Technology Page 197

    Infinitemetallicscreen

    A-- --Øsr :I

    ••

    A z •

    •• •

    il 1 1• ••

    •I -÷:

    •• A4—

    I :

    # N•

    , • •, a

    1 TT1

    b N

    1

    I".. 1

    0: 44-1". 11 Jr....4o.

    I II

    0

    b 1•1 0 •-4----, •• • •

    ••#1 • ,• •

    I•• •

    • •

    I••

    •• •

    • 4•11---'•

    LiI

    #K •••

    • ••••

    •• i

    ••

    • 1 •• •

    I •••

    Half-space

    Fig.2 Approximation of the horn geometry by cascaded step discontinuities.

  • 0.00

    -20.

    -25.-90. -75. -60. -45. -30. 45. 0.00 15. 30. 45. 60. 75. 90.

    Page 198 First International Symposium on Spaee Terahertz Technology

    FAR-FIELD

    THETA (DEG)

    Aperture Dimensions -

    1.45 A X 1.45 A

    Flaring Angles

    70°

    Diplole Polarization

    Vertical (along y-axis,,

    Dipole Position

    0.38A from apex

    Fig.3 Far-field.

  • First International Symposium on Space Terahertz Technology Page 199

    MAGNITUDE OF E-FIELD ALONG APERTURE DIAGONAL1.00

    0.90

    0.80

    0.70

    060

    0.50

    .

    0.40

    0.30

    0.20

    0.10

    0.000.000 0.210 0.420 0.630 0.840 1.050 1.260 1.470 1.680 1.890 2.100

    distance along aperture diagonal

    Fig.4 Magnitude of aperture field. (a) The co-polarazized field. (b) The

    cross-polarized field. (c) Comparison of the co-polar and cross-polar magni-

    tude along the aperture diagonal.

  • Page 200 First International Symposium on Space Terahertz Technology

    phaso(Ey)

    PHASE OF E -FIELD ALONG APERTURE Y-AXIS360. - - -330.

    300.

    210.

    240.

    180.

    150.

    120. "•

    Ey

    7

    7

    270.

    90. Ex6o. -30.

    0.000 0.145 0.290 0.435 0.580 0.725 0.870 1.015 1.160 1.305 1.450

    distance along y-axis (wavelengths)

    Fig.5 Phase of aperture field. (a) The co-polarized field. (b) The cross-

    polarized field. (c) Comparison of the co-polar and cross-polar phase along

    the aperture diagonal.